Dynamic modeling using system identification and attitude control design of GaneFly flapping wings micro aerial vehicle (FWMAV)

2017 ◽  
Author(s):  
R. S. Brian Benyamin ◽  
Muhammad Aldo Aditiya Nugroho ◽  
A. Yosua Sepri ◽  
Bambang Riyanto Trilaksono ◽  
Agoes Moelyadi
Keyword(s):  
System Identification ◽  
Dynamic Modeling ◽  
Attitude Control ◽  
Control Design ◽  
Flapping Wings ◽  
Micro Aerial Vehicle ◽  
Aerial Vehicle

Robust attitude control design for a low-cost hexarotor micro aerial vehicle

2016 ◽  
Vol 38 (6) ◽  
pp. 701-721 ◽  
Author(s):  
Dafizal Derawi ◽  
Nurul Dayana Salim ◽  
Hairi Zamzuri ◽  
Mohd Azizi Abdul Rahman ◽  
Kenzo Nonami
Keyword(s):  
Attitude Control ◽  
Low Cost ◽  
Control Design ◽  
Micro Aerial Vehicle ◽  
Aerial Vehicle

Attitude Control of Flapping Wing Micro Aerial Vehicle Based on Double Fuzzy Sliding Mode Control

2012 ◽  
Vol 468-471 ◽  
pp. 704-707
Author(s):  
Sheng Bin Hu ◽  
Wen Hua Lu ◽  
Zhi Yi Chen ◽  
Lei Lei ◽  
Yi Xuan Zhang
Keyword(s):  
Sliding Mode Control ◽  
Attitude Control ◽  
Fuzzy Controller ◽  
Sliding Mode ◽  
Micro Aerial Vehicle ◽  
Fuzzy Sliding Mode Control ◽  
Mode Control ◽  
Control Scheme ◽  
Aerial Vehicle ◽  
Fuzzy Sliding Mode

An adaptive Double Fuzzy Sliding Mode Control scheme for attitude control of Flapping Wing Micro Aerial Vehicle is proposed in this paper. Based on the feedback linearization technique, a sliding mode controller is designed. To faster response speed, a fuzzy controller is designed to adaptively tune the slope of sliding mode surface. To reduce the chattering, another fuzzy controller is designed to adaptively tune the switch part of sliding mode control. The system stability is proved by Lyapunov principle. Simulation results show that the proposed control scheme is effective.

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